View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 32789U 08021G 23086.79998480 .00051669 00000-0 18991-2 0 9990
2 32789 97.3143 109.3235 0009278 69.0011 291.2221 15.27685487814920
| Epoch (UTC): | 27 March 2023 19:11:58 |
| Eccentricity: | 0.0009278 |
| inclination: | 97.3143° |
| perigee height: | 476 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 109.3235° |
| argument of perigee: | 69.0011° |
| revolutions per day: | 15.27685487 |
| mean anomaly at epoch: | 291.2221° |
| orbit number at epoch: | 81492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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